EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD 2020-0149

Jul 7, 2020

Landing Gear — Nose Landing Gear Door Attachment Bolts — Replacement

EASA Airworthiness Directive 2020-0149 is an airworthiness directive addressing the replacement of nose landing gear door attachment bolts on Saab-Fairchild SF340A, SAAB 340B, and SAAB 2000 aeroplanes. The directive targets bolts with part number 7232203-041, identified by specific tracking and work order numbers, which may be affected by hydrogen embrittlement. This AD mandates the replacement of these bolts to ensure continued safe operation of the affected aircraft.

Airworthiness Directive
  • Saab Ab 2000
  • Saab Ab 340
  • Saab-Fairchild SF340A
  • Saab 340B
  • Saab 2000

EASA AD 2020-0148

Jul 6, 2020

Fuel — Low Pressure Shut Off Valve — Inspection

EASA Airworthiness Directive 2020-0148 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aircraft models. It addresses a potential unsafe condition related to fuel leaks from low pressure shut off valves located on engine #1 and engine #2 pylon areas. The directive mandates inspection and corrective actions to prevent possible fuel spillage and fire hazards.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB SAFO20011

Jul 6, 2020

Operations in Oceanic Airspace during the COVID-19 Public Health Emergency

Operations in Oceanic Airspace during the COVID-19 Public Health Emergency is a Safety Alert for Operators (SAFO 20011) issued by the U.S. Federal Aviation Administration. It addresses potential disruptions in Air Traffic Control (ATC) services in oceanic airspace due to COVID-19 related ATC facility shutdowns. The document provides guidance for flightcrews and operators on contingency procedures to maintain safe operations during these interruptions.

Safety Information Bulletin

EASA AD 2020-0139R1

Jul 3, 2020

Stabilizers – Horizontal Tail Plane Lateral Load Fitting Bushings – Inspection

EASA Airworthiness Directive 2020-0139R1 is an updated directive addressing the inspection and potential repair of horizontal tail plane lateral load fitting bushings on Airbus A350-941 and A350-1041 aeroplanes. It applies to all serial numbers except those with Airbus modifications 110669 or 114806 incorporated. The directive mandates repetitive detailed inspections and corrective actions to prevent structural failure due to bushing migration and associated corrosion or fatigue damage.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2020-0147

Jul 2, 2020

Engine Controls — Mixture Control Cable — Operational Restriction / Replacement

EASA Airworthiness Directive 2020-0147 is an airworthiness directive addressing mixture control cable issues on CEAPR DR400 aeroplanes, specifically models DR 400/120, DR 400/140 B, DR 400/180, and DR 400/180 R with certain serial numbers. It targets mixture control cables with Part Number 57.18.52.020 that may have uncripped cable sheaths, potentially causing loss of mixture control and engine shutdown. The directive mandates operational restrictions and replacement of affected parts to ensure continued airworthiness.

Airworthiness Directive
  • Ceapr DR 400
  • CEAPR DR400/120
  • CEAPR DR400/140 B
  • CEAPR DR400/180
  • CEAPR DR400/180 R

EASA AD 2020-0146

Jul 2, 2020

Main Rotor — Main Rotor Hub — Replacement

EASA Airworthiness Directive 2020-0146 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning PZL SW-4 helicopters. It addresses the replacement of main rotor hubs (MRH) equipped with specific bearings and inserts that have been found to wear prematurely. The directive applies to all serial numbers of PZL SW-4 helicopters and focuses on ensuring continued safe operation by managing the life limits of affected MRHs.

Airworthiness Directive
  • Wsk Pzl-Swidnik SW4
  • PZL SW-4

EASA AD 2020-0145

Jul 1, 2020

Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification

The document titled 'Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification' is an airworthiness directive applicable to Airbus S.A.S. aircraft models A300, A300-600, and A300-600ST (Beluga). It addresses maintenance procedures related to the main landing gear hinge arm and barrel, focusing on pin replacement, inspection, and spacer modification to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)600ST

EASA SIB 2020-02R5

Jun 30, 2020

WITHDRAWN — RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin 2020-02R5 is an updated guidance document addressing operational recommendations related to the COVID-19 pandemic for national competent authorities, aircraft operators, and aerodrome operators. It provides non-mandatory recommendations to reduce the risk of SARS-CoV-2 spread in aviation operations, emphasizing cleaning, disinfection, and management of potentially infected individuals. The bulletin does not target specific aircraft or engine models but applies broadly to commercial air transport operations.

Safety Information Bulletin

EASA AD US-2020-11-12

Jun 29, 2020

Nacelles / Pylons - Thumbnail Fairing and Mid Strut Fairing Panels - Inspection / Replacement / Modification

Federal Aviation Administration Airworthiness Directive 2020-11-12 is a final rule addressing certain Boeing 737-8 and 737-9 airplanes. It focuses on inspection, replacement, and modification of the thumbnail fairing and mid strut fairing panels on the engine nacelle and strut to ensure proper electrical bonding and shielding against high intensity radiated fields (HIRF). This directive aims to prevent potential dual-engine power loss and misleading propulsion parameter displays.

Airworthiness Directive
  • Boeing 73789

EASA AD CF-2020-23

Jun 26, 2020

Ice and Rain Protection — Wing Anti-Ice System — Piccolo Duct Holes Not Conforming to Drawing Requirements

Canadian Airworthiness Directive CF-2020-23 addresses non-conforming piccolo duct holes in the wing anti-ice system of MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, and CL-600-2D24. The directive identifies specific serial numbers affected by manufacturing deviations in piccolo duct bleed holes that could impair wing anti-ice protection. This AD mandates inspection and replacement of affected piccolo duct assemblies to ensure continued airworthiness.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • MHI RJ Aviation ULC CL-600-2C10
  • MHI RJ Aviation ULC CL-600-2C11
  • MHI RJ Aviation ULC CL-600-2D24

EASA AD 2020-0143

Jun 25, 2020

Engine Controls — Push-pull Control and Beta Switch — Inspection / Replacement

EASA Airworthiness Directive 2020-0143 is an airworthiness directive addressing engine controls, specifically the push-pull control and beta switch, for GE Aviation Czech H80-200 and H85-200 engines installed on Aircraft Industries L 410 UVP-E20, L 410 UVP-E20 CARGO, and L 410 NG aeroplanes. The directive mandates inspections, adjustments, and replacements of specific push-pull control parts and beta switches to ensure safe engine operation and prevent uncommanded propeller reverse thrust. It applies to various engine groups defined by part numbers and configurations.

Airworthiness Directive
  • Ge Aviation Czech H75, H80, H85
  • Aircraft Industries L 410 UVP-E20
  • Aircraft Industries L 410 UVP-E20 CARGO
  • Aircraft Industries L 410 NG

EASA SD SD-2020-03

Jun 25, 2020

Superseded by EASA SD-2021-04

EASA Safety Directive 2020-03 is a regulatory document issued to establish operational measures aimed at preventing the spread of the coronavirus SARS-CoV-2 in commercial air transport. It applies to aircraft operators certified under Commission Regulation (EU) 965/2012 and focuses on cleaning and disinfecting aircraft surfaces to minimize COVID-19 transmission risks. The directive addresses all commercial passenger flights, with specific attention to long haul flights lasting six hours or more.

Safety Directive

EASA SD SD-2020-04

Jun 25, 2020

Superseded by EASA SD-2021-05

EASA Safety Directive 2020-04 is a regulatory document issued to Third Country Operators authorized by EASA to perform commercial air transport of passengers to, from, or within the European Union. It mandates operational measures to prevent the spread of the coronavirus SARS-CoV-2, focusing on cleaning and disinfection protocols for aircraft. The directive applies to all relevant commercial passenger flights, including long haul flights, to mitigate COVID-19 transmission risks onboard aircraft.

Safety Directive

EASA AD 2020-0142

Jun 25, 2020

Tail Rotor Drive — Slider Assembly Pitch Control — Inspection / Replacement

The document titled 'Tail Rotor Drive — Slider Assembly Pitch Control — Inspection / Replacement' is an airworthiness directive applicable to LEONARDO S.p.A. HELICOPTERS models A109 and A119. It addresses inspection and replacement procedures for the tail rotor drive slider assembly pitch control components to ensure continued airworthiness and safety. The directive provides guidance on maintaining the integrity of these critical helicopter parts.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters A109
  • Leonardo S.P.A. Helicopters A119
  • Leonardo A109
  • Leonardo A119

EASA AD 2020-0036R1

Jun 24, 2020

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementation

EASA Airworthiness Directive 2020-0036R1 is an updated regulatory requirement issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aircraft models. It mandates compliance with the Airworthiness Limitations Section (ALS) Part 2, which includes damage tolerant airworthiness limitation items essential for continued airworthiness. This directive ensures operators maintain the structural integrity of these aircraft by following specified maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD US-2020-11-01

Jun 23, 2020

Flight Controls - Primary Flight Control Actuation System Remote Electronics Unit - Software Update

The document titled "Flight Controls - Primary Flight Control Actuation System Remote Electronics Unit - Software Update" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2020-11-01. It applies to Gulfstream Aerospace Corporation Model GVI airplanes, also known as G650 and G650ER. The AD addresses a safety issue related to the primary flight control actuation system's linear variable displacement transducer (LVDT) mechanical disconnect monitor, which may fail to disconnect affected control surfaces during a failure event.

Airworthiness Directive
  • Gulfstream Aerospace Corporation GVI
  • Gulfstream GVI

EASA AD 2017-0089R1

Jun 23, 2020

Main Rotor — Main Rotor Mast Upper Bearing — Lubrication / Main Rotor Mast Jet Oil Hose — Inspection

EASA Airworthiness Directive 2017-0089R1 is an updated regulatory requirement addressing the lubrication and inspection of the main rotor mast upper bearing and main rotor mast jet oil hose on Airbus Helicopters AS 350, AS 355, and EC 130 models. It specifically targets main rotor mast jet oil hoses with Part Number 704A34-412-015 manufactured in or before the second trimester of 2017. The directive mandates inspections and potential replacements to prevent bearing lubrication failure.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters AS 355

EASA AD 2020-0140

Jun 23, 2020

Propeller — Gearbox Tooth Belt — Inspection / Time Limits / Maintenance Checks — Airworthiness Limitations Section Chapter 4 — Amendment

EASA Airworthiness Directive 2020-0140 is an amendment addressing the inspection, time limits, and maintenance checks of the propeller gearbox tooth belt on Stemme AG TSA-M powered sailplanes (models S6 and S6-RT) and ASP S15-1 aeroplanes. It mandates inspection and possible re-identification of the tooth belts, along with implementation of revised life limits as specified in the applicable Airworthiness Limitations Section (ALS) of the Stemme Aircraft Maintenance Manual. This directive ensures continued airworthiness by updating maintenance requirements for these specific aircraft models.

Airworthiness Directive
  • Stemme Ag ASP
  • Stemme Ag TSA-M
  • Stemme AG TSA-M S6RT
  • ASP S15-1